This report contains the results of a program concerned with the design, construction, and flight testing of a highperformance static electricity discharging system for helicopters. Flight test data showed that the discharging system kept the electrostatic energy of a CH-37 helicopter below 1 millijoule for natural charging currents of up to 50 microamperes. This is in accordance with the established design specifications. Data were also obtained on the radio interference characteristics of the system and on the performance of corona points located in the engine exhaust stream. (Author)
A High-Performance Electrostatic Discharger for Helicopters
1963
2 pages
Report
No indication
English
STATIC DISCHARGER, AIRCRAFT AND INSTALLATION PROCESS FOR THE STATIC DISCHARGER
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